Division [9A] Systems, Equipment and ComponentsF1
United Kingdom
NB:For propulsion systems designed or rated against neutron or transient ionizing radiation, SEE THE MILITARY GOODS CONTROLS.
- [9A001]Aero gas turbine engines having any of the following:
- [9A002]‘Marine gas turbine engines’ designed to use liquid fuel and having all of the following, and specially designed assemblies and components therefor:
- [9A003]Specially designed assemblies or components, incorporating any of the "technologies" specified in 9E003.a., 9E003.h. or 9E003.i. or 9E003.k., for any of the following aero gas turbine engines:
- [9A004]Space launch vehicles, "spacecraft", "spacecraft buses", "spacecraft mission equipment", "spacecraft" on-board systems or equipment, terrestrial equipment, air-launch platforms and “sub-orbital craft” as follows:
- [9A005]Liquid rocket propulsion systems containing any of the systems or components, specified in 9A006.
- [9A006]Systems and components, specially designed for liquid rocket propulsion systems, as follows:
- [9A007]Solid rocket propulsion systems having any of the following:
- [9A008]Components specially designed for solid rocket propulsion systems, as follows:
- [9A009]Hybrid rocket propulsion systems having any of the following:
- [9A010]Specially designed components, systems and structures, for launch vehicles, launch vehicle propulsion systems or "spacecraft", as follows:
- [9A011]Ramjet, scramjet or ‘combined cycle engines’, and specially designed components therefor.
- [9A012]"Unmanned aerial vehicles" ("UAVs"), unmanned "airships", related equipment and components, as follows:
- [9A101]Turbojet and turbofan engines, other than those specified in 9A001, as follows;
- [9A102]‘Turboprop engine systems’ specially designed for unmanned aerial vehicles specified in 9A012 or 9A112.a., and specially designed components therefor, having a ‘maximum power’ greater than 10 kW.
- [9A104]Sounding rockets, capable of a range of at least 300 km.
- [9A105]Liquid propellant rocket engines or gel propellant rocket motors, as follows:
- [9A106]Systems or components, other than those specified in 9A006 as follows, specially designed for liquid rocket propulsion or gel propellant rocket systems:
- [9A107]Solid propellant rocket motors, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A007, having total impulse capacity equal to or greater than 0,841 MNs.
- [9A108]Components, other than those specified in 9A008, as follows, specially designed for solid and hybrid rocket propulsion systems:
- [9A109]Hybrid rocket motors and specially designed components as follows:
- [9A110]Composite structures, laminates and manufactures thereof, other than those specified in 9A010, specially designed for use in ‘missiles’ or the subsystems specified in 9A005, 9A007, 9A105, 9A106.c., 9A107, 9A108.c., 9A116 or 9A119.
- [9A111]Pulse jet or detonation engines, usable in "missiles" or unmanned aerial vehicles specified in 9A012 or 9A112.a., and specially designed components therefor.
- [9A112]"Unmanned Aerial Vehicles" ("UAVs"), other than those specified in 9A012, as follows:
- [9A115]Launch support equipment as follows:
- [9A116]Reentry vehicles, usable in "missiles", and equipment designed or modified therefor, as follows:
- [9A117]Staging mechanisms, separation mechanisms, and interstages, usable in "missiles".
- [9A118]Devices to regulate combustion usable in engines, which are usable in "missiles" or “Unmanned Aerial Vehicles” (“UAVs”) capable of a range of 300 km specified in 9A012 or 9A112.a., specified in 9A011 or 9A111.
- [9A119]Individual rocket stages, usable in complete rocket systems or “Unmanned Aerial Vehicles” (“UAVs”) , capable of a range of 300 km, other than those specified in 9A005, 9A007, 9A009, 9A105, 9A107 and 9A109.
- [9A120]Liquid or gel propellant tanks, other than those specified in 9A006, specially designed for propellants specified in 1C111 or ‘other liquid or gel propellants’ used in rocket systems capable of delivering at least a 500 kg payload to a range of at least 300 km.
- [9A121]Umbilical and interstage electrical connectors specially designed for "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
- [9A350]Spraying or fogging systems, specially designed or modified for fitting to aircraft, "lighter-than-air vehicles" or “Unmanned Aerial Vehicles” (“UAVs”), and specially designed components therefor, as follows: